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V/STOL Aircraft Engine and Mechanical Drive Component Integration
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Sector:
Event:
Aerospace Meeting
Language:
English
Abstract
V/STOL aircraft propulsion systems are required to provide vertical lift, horizontal thrust, attitude control, and distribution of power for engine-out cases with high efficiency, low weight, and high reliability. These V/STOL requirements have been converted into specific design objectives for mechanical drive components including the gears, bearings, clutches, and shafting that interconnect the engines, lift and propulsion fans, and rotors in various V/STOL aircraft defined in recent system studies.
Authors
Topic
Citation
Hudson, S. and Beam, P., "V/STOL Aircraft Engine and Mechanical Drive Component Integration," SAE Technical Paper 781038, 1978, https://doi.org/10.4271/781038.Also In
References
- Spencer J. W. “X-22A Past, Present and Future,” Proceedings of V/STOL Technology and Planning Conference USAF FDL September 1969
- Traskes R. “USN/FMOD FRG VAK-191B Joint Flight Test Program,” NavAir-IR-76 August 1976
- Migdal D. Kress R. “Design and Development of a Multi-Purpose V/STOL Aircraft,” AIAA Paper 77-571 June 1977
- Ames L. E. “How Requirements Influence the Lift/Cruise Fan Aircraft,” SAE Paper 751101 November 1975
- Lampard G. “The Effect of Thrust Vectoring and Attitude Control Concepts on the Propulsion System of V/STOL Aircraft,” AIAA Paper 78-1020 August 1978
- Taha Ettles MacPherson “The Rigidity and Performance of A Helicopter Gearbox with A Cantilevered Housing and Two Taper Roller Bearings,” ASME Paper 77-DET-103 October 1977
- Thomas W. H. “A Clutch for V/STOL,” SAE Paper 770964 November 1977